View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 62410U 26145.58335647 +.00000000 +00000-0 -81907-3 0 00004
2 62410 43.0007 64.5526 0001649 265.7599 311.9333 15.70864510 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001649 |
| inclination: | 43.0007° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 64.5526° |
| argument of perigee: | 265.7599° |
| revolutions per day: | 15.70864510 |
| mean anomaly at epoch: | 311.9333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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